JPS57126504A - Mounting of rotor blade to rotor disc and fan shaped lock pin - Google Patents

Mounting of rotor blade to rotor disc and fan shaped lock pin

Info

Publication number
JPS57126504A
JPS57126504A JP56205068A JP20506881A JPS57126504A JP S57126504 A JPS57126504 A JP S57126504A JP 56205068 A JP56205068 A JP 56205068A JP 20506881 A JP20506881 A JP 20506881A JP S57126504 A JPS57126504 A JP S57126504A
Authority
JP
Japan
Prior art keywords
rotor
mounting
lock pin
shaped lock
fan shaped
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP56205068A
Other languages
Japanese (ja)
Other versions
JPH0233844B2 (en
Inventor
Buruumen Kuroodeio
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of JPS57126504A publication Critical patent/JPS57126504A/en
Publication of JPH0233844B2 publication Critical patent/JPH0233844B2/ja
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/32—Locking, e.g. by final locking blades or keys
    • F01D5/326—Locking of axial insertion type blades by other means
JP56205068A 1980-12-19 1981-12-17 Mounting of rotor blade to rotor disc and fan shaped lock pin Granted JPS57126504A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/218,241 US4389161A (en) 1980-12-19 1980-12-19 Locking of rotor blades on a rotor disk

Publications (2)

Publication Number Publication Date
JPS57126504A true JPS57126504A (en) 1982-08-06
JPH0233844B2 JPH0233844B2 (en) 1990-07-31

Family

ID=22814321

Family Applications (1)

Application Number Title Priority Date Filing Date
JP56205068A Granted JPS57126504A (en) 1980-12-19 1981-12-17 Mounting of rotor blade to rotor disc and fan shaped lock pin

Country Status (9)

Country Link
US (1) US4389161A (en)
JP (1) JPS57126504A (en)
BE (1) BE891325A (en)
CH (1) CH658701A5 (en)
DE (1) DE3148984A1 (en)
FR (1) FR2501283B1 (en)
GB (1) GB2089899B (en)
IT (1) IT1142138B (en)
SE (1) SE450843B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010112376A (en) * 2008-11-05 2010-05-20 General Electric Co <Ge> Turbine with interrupted purge flow

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2519692B1 (en) * 1982-01-14 1986-08-22 Snecma DEVICE FOR AXIAL LOCKING OF TURBINE BLADES AND COMPRESSORS
FR2524933B1 (en) * 1982-04-13 1987-02-20 Snecma AXIAL LOCKING DEVICE FOR TURBINE OR COMPRESSOR ROTOR BLADES
US4489468A (en) * 1982-06-24 1984-12-25 Elliott Turbomachinery Co., Inc. Method of providing a multivalve turbine nozzle ring interface seal
FR2603333B1 (en) * 1986-09-03 1990-07-20 Snecma TURBOMACHINE ROTOR COMPRISING A MEANS OF AXIAL LOCKING AND SEALING OF BLADES MOUNTED IN AXIAL PINS OF THE DISC AND MOUNTING METHOD
US4868963A (en) * 1988-01-11 1989-09-26 General Electric Company Stator vane mounting method and assembly
DE3818466C1 (en) * 1988-05-31 1989-12-21 Mtu Muenchen Gmbh
FR2637321B1 (en) * 1988-10-05 1990-11-30 Snecma TURBOMACHINE ROTOR PROVIDED WITH A BLADE FIXING DEVICE
US4895490A (en) * 1988-11-28 1990-01-23 The United States Of America As Represented By The Secretary Of The Air Force Internal blade retention system for rotary engines
US5131814A (en) * 1990-04-03 1992-07-21 General Electric Company Turbine blade inner end attachment structure
US5112193A (en) * 1990-09-11 1992-05-12 Pratt & Whitney Canada Fan blade axial retention device
US5139389A (en) * 1990-09-14 1992-08-18 United Technologies Corporation Expandable blade root sealant
US5137420A (en) * 1990-09-14 1992-08-11 United Technologies Corporation Compressible blade root sealant
US5256035A (en) * 1992-06-01 1993-10-26 United Technologies Corporation Rotor blade retention and sealing construction
US5411369A (en) * 1994-02-22 1995-05-02 Pratt & Whitney Canada, Inc. Gas turbine engine component retention
US5476366A (en) * 1994-09-20 1995-12-19 Baldor Electric Co. Fan construction and method of assembly
DE19507673C2 (en) * 1995-03-06 1997-07-03 Mtu Muenchen Gmbh Guide wheel for turbomachinery
GB2313162B (en) * 1996-05-17 2000-02-16 Rolls Royce Plc Bladed rotor
GB9925261D0 (en) * 1999-10-27 1999-12-29 Rolls Royce Plc Locking devices
DE10128505C2 (en) * 2001-06-14 2003-04-30 Mtu Aero Engines Gmbh Attachment of blades
US6776583B1 (en) * 2003-02-27 2004-08-17 General Electric Company Turbine bucket damper pin
US20060067822A1 (en) * 2004-09-24 2006-03-30 D Anna Frank P Pitch lock and lag positioner for a rotor blade folding system
US20060120873A1 (en) * 2004-12-03 2006-06-08 Sikorsky Aircraft Corporation Damper positioner for a rotor blade folding system
WO2006106734A1 (en) * 2005-03-30 2006-10-12 Zephyr Corporation Windmill
US7530791B2 (en) * 2005-12-22 2009-05-12 Pratt & Whitney Canada Corp. Turbine blade retaining apparatus
US7530790B2 (en) * 2006-09-20 2009-05-12 Sikorsky Aircraft Corporation Rotor blade folding system
US8038394B2 (en) * 2008-01-16 2011-10-18 Sikorsky Aircraft Corporation System and method of damping a 1P motion
US8251668B2 (en) * 2009-06-30 2012-08-28 General Electric Company Method and apparatus for assembling rotating machines
FR2961847B1 (en) * 2010-06-25 2012-08-17 Snecma AUBES MOBILE WHEEL IN COMPOSITE MATERIAL FOR A TURBINE GAS TURBINE ENGINE WITH A WAVEBASE / TIGHTENING DISC
FR2963383B1 (en) * 2010-07-27 2016-09-09 Snecma DUST OF TURBOMACHINE, ROTOR, LOW PRESSURE TURBINE AND TURBOMACHINE EQUIPPED WITH SUCH A DAWN
FR2988128A1 (en) * 2012-03-19 2013-09-20 Alstom Technology Ltd TURBINE ROTOR FOR A THERMOELECTRIC POWER PLANT
US10638763B2 (en) * 2017-07-05 2020-05-05 Masontops, Inc. Bread lame
US11038394B2 (en) 2018-01-25 2021-06-15 Ge Aviation Systems Llc Generator rotor with coil end-turn retention mechanism
CN109098777A (en) * 2018-09-05 2018-12-28 中国航发动力股份有限公司 A kind of flue gas turbine expander disc slot is to connection structure and its application method

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1303090A (en) * 1919-05-06 Thomas mcceay
US1072457A (en) * 1912-01-30 1913-09-09 Westinghouse Machine Co Blade-mounting.
BE501031A (en) * 1950-02-03
US2713991A (en) * 1951-05-05 1955-07-26 A V Roe Canada Ltd Rotor blade locking device
GB712112A (en) * 1951-07-13 1954-07-21 Bristol Aeroplane Co Ltd Improvements in or relating to blade-locking means for turbine and the like rotor assemblies
DE1070335B (en) * 1955-06-24
US2994507A (en) * 1959-01-23 1961-08-01 Westinghouse Electric Corp Blade locking structure
GB1291302A (en) * 1970-03-14 1972-10-04 Sec Dep For Defendence Improvements in bladed rotor assemblies
US3656865A (en) * 1970-07-21 1972-04-18 Gen Motors Corp Rotor blade retainer
GB1479332A (en) * 1974-11-06 1977-07-13 Rolls Royce Means for retaining blades to a disc or like structure
DE2533044A1 (en) * 1975-07-24 1977-02-10 Metallgesellschaft Ag Quick release clamping pin - has tapered wedge located in slot in guide pin retained by end stops

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010112376A (en) * 2008-11-05 2010-05-20 General Electric Co <Ge> Turbine with interrupted purge flow

Also Published As

Publication number Publication date
JPH0233844B2 (en) 1990-07-31
GB2089899B (en) 1984-09-05
US4389161A (en) 1983-06-21
BE891325A (en) 1982-03-31
FR2501283A1 (en) 1982-09-10
SE8107451L (en) 1982-06-20
DE3148984C2 (en) 1993-05-27
CH658701A5 (en) 1986-11-28
IT1142138B (en) 1986-10-08
IT8125688A0 (en) 1981-12-18
SE450843B (en) 1987-08-03
FR2501283B1 (en) 1986-12-05
GB2089899A (en) 1982-06-30
DE3148984A1 (en) 1982-07-22

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